EP3048307B1 - Method for controlling a rotational speed of a fan - Google Patents

Method for controlling a rotational speed of a fan Download PDF

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Publication number
EP3048307B1
EP3048307B1 EP16151537.4A EP16151537A EP3048307B1 EP 3048307 B1 EP3048307 B1 EP 3048307B1 EP 16151537 A EP16151537 A EP 16151537A EP 3048307 B1 EP3048307 B1 EP 3048307B1
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EP
European Patent Office
Prior art keywords
drive
rotational speed
speed
virtual
target rotational
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Not-in-force
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EP16151537.4A
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German (de)
French (fr)
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EP3048307A1 (en
Inventor
Gerold Schultheiss
Alexander Spies
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Mahle International GmbH
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Mahle International GmbH
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Publication of EP3048307A1 publication Critical patent/EP3048307A1/en
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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D25/00Pumping installations or systems
    • F04D25/02Units comprising pumps and their driving means
    • F04D25/06Units comprising pumps and their driving means the pump being electrically driven
    • F04D25/0606Units comprising pumps and their driving means the pump being electrically driven the electric motor being specially adapted for integration in the pump
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01PCOOLING OF MACHINES OR ENGINES IN GENERAL; COOLING OF INTERNAL-COMBUSTION ENGINES
    • F01P7/00Controlling of coolant flow
    • F01P7/02Controlling of coolant flow the coolant being cooling-air
    • F01P7/04Controlling of coolant flow the coolant being cooling-air by varying pump speed, e.g. by changing pump-drive gear ratio
    • F01P7/042Controlling of coolant flow the coolant being cooling-air by varying pump speed, e.g. by changing pump-drive gear ratio using fluid couplings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01PCOOLING OF MACHINES OR ENGINES IN GENERAL; COOLING OF INTERNAL-COMBUSTION ENGINES
    • F01P7/00Controlling of coolant flow
    • F01P7/02Controlling of coolant flow the coolant being cooling-air
    • F01P7/04Controlling of coolant flow the coolant being cooling-air by varying pump speed, e.g. by changing pump-drive gear ratio
    • F01P7/048Controlling of coolant flow the coolant being cooling-air by varying pump speed, e.g. by changing pump-drive gear ratio using electrical drives
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D25/00Pumping installations or systems
    • F04D25/02Units comprising pumps and their driving means
    • F04D25/022Units comprising pumps and their driving means comprising a yielding coupling, e.g. hydraulic
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D27/00Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
    • F04D27/004Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids by varying driving speed
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01PCOOLING OF MACHINES OR ENGINES IN GENERAL; COOLING OF INTERNAL-COMBUSTION ENGINES
    • F01P2025/00Measuring
    • F01P2025/60Operating parameters
    • F01P2025/64Number of revolutions
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02BCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO BUILDINGS, e.g. HOUSING, HOUSE APPLIANCES OR RELATED END-USER APPLICATIONS
    • Y02B30/00Energy efficient heating, ventilation or air conditioning [HVAC]
    • Y02B30/70Efficient control or regulation technologies, e.g. for control of refrigerant flow, motor or heating

Definitions

  • the invention relates to a method for controlling a speed of a fan of a fan to a target speed, which is driven jointly by a first drive and a second drive, wherein the first drive is controlled and / or controlled by a first control unit and the second drive is controlled and / or controlled by a second control unit.
  • the present invention is based on the object to provide an improved or at least other embodiment of a method for controlling a speed of a fan wheel, which is driven by two drives, which is characterized in particular by an improved efficiency.
  • the invention is based on the general idea of enabling an efficiency-optimized power split between the first drive and the second drive. This is achieved by determining, based on an efficiency strategy, a first torque to be generated by the first drive and a second torque to be generated by the second drive, in each case starting from the first torque and from the second torque Torque a first virtual target speed and a second virtual target speed are determined, and that the first virtual target speed of the first control unit is supplied as an input and that the second virtual target speed of the second control unit is supplied as an input variable.
  • the efficiency strategy divides the torque required to achieve the desired speed of the fan wheel into the first drive and the second drive such that the overall efficiency is improved.
  • a virtual speed is understood to mean a value that is used only as an auxiliary quantity.
  • virtual target speeds are values that are actually not to be reached. Accordingly, virtual actual speeds are not available in the system.
  • the virtual speeds indicate to the control units operating conditions that are not actually present to achieve the desired torque distributions between the two drives.
  • a favorable possibility provides that an electric motor as the first drive and a viscous coupling are used as a second drive, which the fan coupled to a shaft of the internal combustion engine.
  • This allows the advantages of the electric motor and the viscous coupling to be well combined.
  • the high dynamics of the electric motor can be used to allow rapid achievement of the desired speed.
  • the efficiency characteristics of the two drives are different, so that an optimization of the overall efficiency can be achieved by a power distribution between the two drives. For example, at an operating point at which one drive is more efficient, it takes over the drive of the fan wheel entirely or at least to a greater extent than the other less efficient drive.
  • a further favorable possibility provides that the torques to be generated by the first drive and by the second drive are determined by the efficiency strategy on the basis of a desired rotational speed of the fan wheel and / or a rotational speed of a shaft of the internal combustion engine.
  • the efficiency of the viscous coupling is dependent, inter alia, on the difference between the rotational speed of the shaft of the internal combustion engine and the rotational speed of the fan wheel, for example, the slip power of the viscous coupling is greater at high differences, so that the efficiency of the viscous coupling is smaller.
  • the efficiency of the electric drive results from the efficiency chain comprising the efficiencies of the electric motor, the lines, the power amplifier of the engine control and the generator. Based on the target speed of the fan and the speed of the shaft of the engine so it can be determined in what proportion the power of the two drives must be divided to determine an optimal efficiency.
  • a particularly favorable possibility provides that the torques to be generated by the first drive and by the second drive through the efficiency strategy, taking into account the efficiencies of the first drive and the second drive to be determined. Thus, it is possible to optimize the overall efficiency in driving the fan wheel.
  • first virtual setpoint speed and the second virtual setpoint speed are determined by means of a speed-torque characteristic of the fan wheel from the first torque and the second torque.
  • speed-torque characteristic in short characteristic curve, it can be determined which speed the fan wheel would reach if the fan wheel is driven with the first or with the second torque. If this speed is used as the first setpoint speed or second virtual setpoint speed, due to the pilot control maps in the control units, the two drives which attempt to reach the virtual speeds generate just the first torque or the second torque.
  • the generated torques of the drives are not present as a measure, a distribution of the torques can be achieved.
  • a further advantageous solution provides that the first control unit and the second control unit each use a pilot control map and a PID controller. This type of control units has proven itself and allows a fast and efficient control of the speed of the fan wheel.
  • a PID controller is understood to mean a proportional-integral-derivative controller.
  • a particularly advantageous solution provides that the first virtual speed is used as input to the pilot map of the first control unit of the first drive and that the second virtual target speed is used as an input to the pilot map of the second control unit of the second drive.
  • the virtual target speed as an input variable for the pilot control maps of the control units are from the pilot control maps just determines the control variables for the respective drives, which are necessary to achieve the virtual target speeds, so the control variables that generate the first torque and the second torque through the respective drives.
  • a favorable variant provides that the control deviation, which is used by the PID controllers, from a difference between the speed of the fan and the target speed of the fan wheel is determined. In this way it can be achieved that the control units to the correct target speed control, although the control units, the virtual speeds are supplied as an input variable.
  • a further favorable variant provides that the respective control deviations which are used by the PID controllers are determined from a difference between the respective virtual setpoint speed and a respective virtual actual speed.
  • the respective virtual actual speeds are formed from the speed of the fan in the same way as the virtual target speeds from the target speed, so that at a match of the speed of the fan with the target speed and the virtual target speeds with the virtual Actual speeds match. It can thereby be achieved that the first control unit and the second control unit regulate the fan wheel to the desired desired speed.
  • a particularly favorable variant provides that the respective virtual actual rotational speeds are determined by subtracting an offset from the rotational speed, wherein the offset is the difference between the target rotational speed and the respective virtual target rotational speed.
  • the virtual actual rotational speeds can be determined by simple addition or subtraction calculations. So it is only a small amount of computation necessary.
  • the virtual actual rotational speeds are determined by multiplying the rotational speeds by a division factor, wherein the division factor is the quotient of the respective virtual target rotational speed by the target rotational speed.
  • the one drive which is to perform a lower partial power and less involved in the control of the speed of the fan wheel, as by multiplication with the division factor according to the size of the control deviation in relation to the power distribution on the each control units is divided.
  • first control unit and the second control unit are speed control units, or that each speed control units are used as the first control unit and as the second control unit. Speeds can be measured very easily, so that the use of speed control units is cheaper to implement than the use of torque control units.
  • a further advantageous solution provides that the rotational speeds of the first drive and the second drive are coupled.
  • the first drive and the second drive can not rotate independently of each other.
  • a motor vehicle with a fan which is driven by a first drive and by a second drive, wherein a speed of at least one fan of the fan is controlled by a method as described above.
  • the advantages of the method are thus transferred to the motor vehicle, to the above description of which reference is made.
  • a particularly favorable variant provides that the first drive is an electric motor and the second drive is a viscous coupling which couples the fan wheel to an internal combustion engine of the motor vehicle.
  • An in Fig. 1 Arrangement 10 includes an internal combustion engine 12 with a shaft 14. Furthermore, the arrangement comprises a fan 16 with at least one fan 17, which is used for example for cooling the internal combustion engine 12. And driven by a first drive 18 and by a second drive 20.
  • the first drive 18 and the second drive 20 differ, for example, the first drive is an electric motor and the second drive is a viscous coupling which couples the fan 17 with the shaft 14 of the internal combustion engine 12, so that the rotation of the shaft 14 of the internal combustion engine 12 to a Rotation of the fan 17 is transmitted.
  • the first drive 18 has a first control unit 24 and the second drive 20 has a second control unit 26.
  • the first control unit 24 and the second control unit 26 regulate the power of the first drive 18 and the second drive 20 such that the rotational speed 22 of the fan wheel 17 at least approaches a target rotational speed 28.
  • the measurement 23 of the speed 22 can be done for example by a tachometer.
  • the control units 24, 26 each have a PID controller 25 (proportional-integral-differential controller) and a pilot control map 27. Furthermore, control variables 29 for the respective drives are stored in the pilot control map 27, which are necessary for certain operating points of the fan 16. For example, control variables 29 are stored for the steady-state operation as a function of the rotational speed 22 of the fan wheel 17.
  • a target speed 28 at the control units 24, 26 can be determined using the pilot control maps 27, a first good estimate for the correct control variables 29 for the drives, so that the approximation to the actual required control variables 29 can take place more quickly.
  • a determination 30 of the setpoint speed 28 of the fan wheel 17 takes place, for example, by an engine control unit 31, in particular based on a temperature of the internal combustion engine 12 or a temperature of a cooling medium, such as water. At high temperatures, higher target speeds are set for better cooling.
  • an efficiency strategy 32 is applied.
  • the two drives 18, 20 have different efficiencies, in particular different dependencies of the efficiencies, for example, on the speed or the torque to be generated. For this reason, a power distribution which is advantageous for the overall efficiency is different for different operating points.
  • the first drive 18 and the second drive 20 jointly drive the fan 17, so that the rotational speeds of the first drive 18 and the second drive 20 are coupled together.
  • the rotational speeds of the first drive 18 and the second drive 20 are equal to the speed 22 of the fan wheel 17.
  • the first drive 18 must have a first torque 34 and the second drive 20 must apply a second torque 36 to bring the fan 17 to the desired desired speed 28.
  • the first torque 34 and the second torque 36 are converted into a first target virtual speed 38 and a second target virtual speed 40 and used as input to the first control unit 24 and the second control unit 26.
  • the determination of the virtual setpoint rotational speeds 38, 40 from the torques 34, 36 takes place with the aid of a torque / rotational speed characteristic, in short characteristic curve 41, of the fan wheel 17.
  • This characteristic curve 41 can be derived, for example, theoretically from the geometry of the fan 16 or experimentally be determined. From the characteristic curve 41, the torques are known, which are necessary to keep the fan 17 at a certain speed. Accordingly, from the characteristic curve 41, the virtual setpoint rotational speeds 38, 40 can be determined, which would occur if the two drives 18, 20 with the first torque 34 and second torque 36 determined on the basis of the efficiency strategy 32 each drive the fan wheel 17 alone would.
  • the virtual speeds 38, 40 are passed as an input to the control units 24, 26.
  • the control variables 29 for the drives 18, 20 are determined with the aid of the pilot control maps 27, which are required to keep the rotational speed 22 of the fan wheel 17 at the respective virtual desired rotational speeds 38, 40.
  • These control variables 29 cause the drives 18, 20 to determine the torques determined by the efficiency strategy 32 34, 36 generate.
  • the two drives 18 and 20 generate the first torque 34 and the second torque 36 exactly in the ratio determined by the efficiency strategy 32.
  • a determination 42 of the control deviation 44 takes place. Since the control units 24 and 26 are supplied with virtual nominal rotational speeds 38, 40, the determination 42 of the control deviation 44 can not take place in the usual manner, since otherwise the two drives 18, 20 would each regulate to a different speed, so that the two drives 18, 20 would work against each other.
  • the determination 42 of the control deviation 44 therefore takes place by forming the difference between the setpoint speed 28 and the speed 22 of the fan wheel 17.
  • the control deviation 44 is then provided to both control units 24, 26, so that the PID controllers 25 of the control units 24, 26 do not have to make their own determination 42 of the control deviation 44.
  • the two drives 18, 20 can be removed from the operating points, which were set using the virtual target speeds 38, 40. That is, the desired power ratio determined by the efficiency strategy 32 may not be met. However, the deviations remain small, so that the arrangement 10 can still be operated close to the efficiency optimum.
  • setpoint speed 28 is redefined with the aid of the efficiency strategy 32, the correct power ratio is readjusted so that the deviation from the desired power ratio can be accepted for frequent setpoint speed changes.
  • setpoint speed 28 is set again in a specific interval is, although no change in the target speed is provided by the engine control unit.
  • FIG. 3 and FIG. 4 illustrated second embodiment of the method for controlling the speed 22 of the fan 17 differs from that in the Fig. 1 and Fig. 2 shown in the method in that the control deviation 44 within the control units 24, 26 from a difference between the virtual target speeds 38, 40 and virtual actual speeds 46 and 48 is determined.
  • the rotational speed 22 of the fan wheel 17 is converted into a first virtual actual rotational speed 46 and into a second virtual actual rotational speed 48.
  • the first virtual actual rotational speed 46 is supplied to the first control unit 24 and the second virtual actual rotational speed 48 becomes the second control unit 26 is supplied.
  • control deviation 44 is then determined in a conventional manner in the control units 24, 26 by the difference between the virtual target speed and the virtual actual speed. In this way, different control deviations 44 may be determined for the two control units 24, 26 under certain circumstances.
  • the virtual actual rotational speeds 46, 48 must be formed from the rotational speed 22 of the fan wheel 17 such that when the rotational speed 22 of the fan wheel 17 corresponds to the target rotational speed 28, the first virtual actual rotational speed 46 of the first virtual target rotational speed 28 and the second actual virtual speed 48 correspond to the second target virtual speed 40. This can ensure that the two control units 24, 26 control the speed 22 of the fan 17 together to the target speed 28.
  • both control units 24, 26 work together and to regulate the rotational speed 22 of the fan wheel 17 to the desired rotational speed 28.
  • Other possibilities for determining 50 of the virtual actual rotational speed 46, 48 are also conceivable as long as the virtual actual rotational speeds 46, 48 coincide with the virtual target rotational speeds 38, 40 when the rotational speed 22 coincides with the target rotational speed 28.
  • the right in the FIG. 3 and FIG. 4 illustrated second embodiment of the method with regard to sequence and function with in the Fig. 1 and Fig. 2 illustrated first embodiment of the method, to the above description, reference is made in this regard.

Description

Die Erfindung betrifft ein Verfahren zur Regelung einer Drehzahl eines Lüfterrades eines Lüfters auf eine Soll-Drehzahl, das gemeinsam durch einen ersten Antrieb und einen zweiten Antrieb angetrieben wird, wobei der erste Antrieb durch eine erste Regeleinheit geregelt und/oder gesteuert wird und der zweite Antrieb durch eine zweite Regeleinheit geregelt und/oder gesteuert wird.The invention relates to a method for controlling a speed of a fan of a fan to a target speed, which is driven jointly by a first drive and a second drive, wherein the first drive is controlled and / or controlled by a first control unit and the second drive is controlled and / or controlled by a second control unit.

Aus der DE10219872 A1 ist ein Lüfterantrieb mit Flüssigkeitsreibungskupplung und zusätzlichem elektrischen Antrieb bekannt. Die dort offenbarte Regelung beschränkt sich auf die Ausregelung der Regelabweichung zwischen geforderter Soll-Drehzahl und aktueller Lüfterraddrehzahl. Dadurch können die Vorteile des kombinierten Lüfterantriebs nicht vollständig ausgenutzt werden.From the DE10219872 A1 is a fan drive with fluid friction clutch and additional electric drive known. The regulation disclosed therein is limited to the adjustment of the control deviation between the required setpoint speed and the current fan speed. As a result, the benefits of the combined fan drive can not be fully exploited.

Der vorliegenden Erfindung liegt die Aufgabe zu Grunde, eine verbesserte oder zumindest andere Ausführungsform eines Verfahrens zur Regelung einer Drehzahl eines Lüfterrades, welches durch zwei Antriebe angetrieben wird, anzugeben, die sich insbesondere durch einen verbesserten Wirkungsgrad auszeichnet.The present invention is based on the object to provide an improved or at least other embodiment of a method for controlling a speed of a fan wheel, which is driven by two drives, which is characterized in particular by an improved efficiency.

Diese Aufgabe wird erfindungsgemäß durch die unabhängigen Ansprüche gelöst. Vorteilhafte Weiterbildungen sind Gegenstand der abhängigen Ansprüche.This object is achieved by the independent claims. Advantageous developments are the subject of the dependent claims.

Die Erfindung beruht auf dem allgemeinen Gedanken, eine wirkungsgradoptimierte Leistungsverzweigung zwischen dem ersten Antrieb und dem zweiten Antrieb zu ermöglichen. Dies wird dadurch erreicht, dass anhand einer Effizienzstrategie ein vom dem ersten Antrieb zur erzeugendes erstes Drehmoment und ein von dem zweiten Antrieb zu erzeugendes zweites Drehmoment bestimmt werden, dass jeweils ausgehend von dem ersten Drehmoment und von dem zweiten Drehmoment eine erste virtuelle Soll-Drehzahl und eine zweite virtuelle Soll-Drehzahl bestimmt werden, und dass die erste virtuelle Soll-Drehzahl der ersten Regeleinheit als eine Eingangsgröße zugeführt wird und dass die zweite virtuelle Soll-Drehzahl der zweiten Regeleinheit als Eingangsgröße zugeführt wird. Durch die Effizienzstrategie wird das zur Erreichung der Soll-Drehzahl des Lüfterrades benötigte Drehmoment auf den ersten Antrieb und den zweiten Antrieb aufgeteilt, derart, dass der Gesamtwirkungsgrad verbessert ist. Da die erzeugten Drehmomente nicht als Messgröße vorliegen, werden anhand der zu erzeugenden Drehmomente virtuelle Soll-Drehzahlen bestimmt. Diese virtuellen Soll-Drehzahlen werden den Regeleinheiten zugeführt, welche dann mit Hilfe der in den Regeleinheiten hinterlegten Vorsteuerkernfeldern die notwendigen Steuergrößen für die jeweiligen Antriebe ermitteln, und die Antriebe entsprechend steuern. Auf diese Weise wird die gewünschte, für den Wirkungsgrad optimierte, Leistungsverteilung zwischen den beiden Antrieben, annähernd erzielt. Beim Halten der Drehzahl des Lüfterrades auf die Soll-Drehzahl weichen die Regeleinheiten nach einer Einschwingphase nicht wesentlich von den aufgrund der Vorsteuerkernfelder bestimmten Steuergrößen ab, sodass auch im andauernden Betrieb die wirkungsgradoptimierte Leistungsaufteilung zwischen dem ersten Antrieb und dem zweiten Antrieb zumindest annähernd erhalten bleibt.The invention is based on the general idea of enabling an efficiency-optimized power split between the first drive and the second drive. This is achieved by determining, based on an efficiency strategy, a first torque to be generated by the first drive and a second torque to be generated by the second drive, in each case starting from the first torque and from the second torque Torque a first virtual target speed and a second virtual target speed are determined, and that the first virtual target speed of the first control unit is supplied as an input and that the second virtual target speed of the second control unit is supplied as an input variable. The efficiency strategy divides the torque required to achieve the desired speed of the fan wheel into the first drive and the second drive such that the overall efficiency is improved. Since the generated torques are not available as a measured variable, virtual setpoint speeds are determined on the basis of the torques to be generated. These virtual target speeds are fed to the control units, which then determine the necessary control variables for the respective drives with the aid of the pilot control fields stored in the control units, and control the drives accordingly. In this way, the desired, optimized for the efficiency, power distribution between the two drives, approximately achieved. When holding the speed of the fan wheel to the target speed, the control units do not deviate significantly after a transient phase from the control variables determined on the basis of pilot control fields, so that the efficiency-optimized power distribution between the first drive and the second drive remains at least approximately even in continuous operation.

In der Beschreibung und den beigefügten Ansprüchen wird unter einer virtuellen Drehzahl ein Wert verstanden, der nur als Hilfsgröße verwendet wird. Beispielsweise sind virtuelle Solldrehzahlen Werte, die tatsächlich gar nicht erreicht werden sollen. Entsprechend sind virtuelle Ist-Drehzahlen nicht im System vorhanden. Die virtuellen Drehzahlen zeigen den Regeleinheiten Betriebszustände an, die tatsächlich nicht vorhanden sind, um die gewünschten Drehmomentverteilungen zwischen den beiden Antrieben zu erzielen.In the specification and the appended claims, a virtual speed is understood to mean a value that is used only as an auxiliary quantity. For example, virtual target speeds are values that are actually not to be reached. Accordingly, virtual actual speeds are not available in the system. The virtual speeds indicate to the control units operating conditions that are not actually present to achieve the desired torque distributions between the two drives.

Eine günstige Möglichkeit sieht vor, dass ein Elektromotor als erster Antrieb und eine Viscokupplung als zweiter Antrieb verwendet werden, welche das Lüfterrad an eine Welle der Brennkraftmaschine ankoppelt. Dadurch können die Vorteile des Elektromotors und der Viscokupplung gut miteinander kombiniert werden. Insbesondere kann die hohe Dynamik des Elektromotors genutzt werden, um ein schnelles Erreichen der Soll-Drehzahl zu ermöglichen. Des Weiteren sind die Wirkungsgradkennlinien der beiden Antriebe unterschiedlich, sodass durch eine Leistungsaufteilung zwischen den beiden Antrieben eine Optimierung des Gesamtwirkungsgrades erzielt werden kann. Beispielsweise übernimmt an einem Arbeitspunkt, an dem der eine Antrieb effizienter ist, dieser den Antrieb des Lüfterrades ganz oder zumindest zu einem größeren Teil als der andere weniger effiziente Antrieb.A favorable possibility provides that an electric motor as the first drive and a viscous coupling are used as a second drive, which the fan coupled to a shaft of the internal combustion engine. This allows the advantages of the electric motor and the viscous coupling to be well combined. In particular, the high dynamics of the electric motor can be used to allow rapid achievement of the desired speed. Furthermore, the efficiency characteristics of the two drives are different, so that an optimization of the overall efficiency can be achieved by a power distribution between the two drives. For example, at an operating point at which one drive is more efficient, it takes over the drive of the fan wheel entirely or at least to a greater extent than the other less efficient drive.

Eine weitere günstige Möglichkeit sieht vor, dass die von dem ersten Antrieb und von dem zweiten Antrieb zu erzeugenden Drehmomente durch die Effizienzstrategie anhand einer Soll-Drehzahl des Lüfterrades und/oder einer Drehzahl einer Welle der Brennkraftmaschine bestimmt werden. Der Wirkungsgrad der Viscokupplung ist beispielsweise unter anderem abhängig von der Differenz zwischen der Drehzahl der Welle der Brennkraftmaschine und der Drehzahl des Lüfterrades, beispielsweise ist bei hohen Differenzen die Schlupfleistung der Viscokupplung größer, sodass der Wirkungsgrad der Viscokupplung kleiner ist. Der Wirkungsgrad des elektrischen Antriebs ergibt sich aus der Wirkungsgradkette umfassend die Wirkungsgrade des Elektromotors, der Leitungen, der Endstufe der Motorsteuerung sowie des Generators. Anhand der Soll-Drehzahl des Lüfterrades und der Drehzahl der Welle der Brennkraftmaschine kann also bestimmt werden, in welchem Verhältnis die Leistung der beiden Antriebe aufgeteilt werden muss, um einen optimalen Wirkungsgrad zu bestimmen.A further favorable possibility provides that the torques to be generated by the first drive and by the second drive are determined by the efficiency strategy on the basis of a desired rotational speed of the fan wheel and / or a rotational speed of a shaft of the internal combustion engine. The efficiency of the viscous coupling is dependent, inter alia, on the difference between the rotational speed of the shaft of the internal combustion engine and the rotational speed of the fan wheel, for example, the slip power of the viscous coupling is greater at high differences, so that the efficiency of the viscous coupling is smaller. The efficiency of the electric drive results from the efficiency chain comprising the efficiencies of the electric motor, the lines, the power amplifier of the engine control and the generator. Based on the target speed of the fan and the speed of the shaft of the engine so it can be determined in what proportion the power of the two drives must be divided to determine an optimal efficiency.

Eine besonders günstige Möglichkeit sieht vor, dass die von dem ersten Antrieb und von dem zweiten Antrieb zu erzeugenden Drehmomente durch die Effizienzstrategie unter Berücksichtigung der Wirkungsgrade des ersten Antriebs und des zweiten Antriebs bestimmt werden. Somit ist es möglich, den Gesamtwirkungsgrad beim Antreiben des Lüfterrades zu optimieren.A particularly favorable possibility provides that the torques to be generated by the first drive and by the second drive through the efficiency strategy, taking into account the efficiencies of the first drive and the second drive to be determined. Thus, it is possible to optimize the overall efficiency in driving the fan wheel.

Eine vorteilhafte Lösung sieht vor, dass die erste virtuelle Soll-Drehzahl und die zweite virtuelle Soll-Drehzahl mit Hilfe einer Drehzahl-Drehmoment-Kennlinie des Lüfterrades aus dem ersten Drehmoment bzw. dem zweiten Drehmoment bestimmt werden. Anhand der bekannten Drehzahl-Drehmoment-Kennlinie, kurz Kennlinie, kann ermittelt werden, welche Drehzahl das Lüfterrad erreichen würde, wenn das Lüfterrad mit dem ersten bzw. mit dem zweiten Drehmoment angetrieben wird. Wird diese Drehzahl als erste Soll-Drehzahl bzw. zweite virtuelle Soll-Drehzahl verwendet, werden aufgrund der Vorsteuerkennfelder in den Regeleinheiten die beiden Antriebe, welche versuchen die virtuellen Drehzahlen zu erreichen, gerade das erste Drehmoment bzw. das zweite Drehmoment erzeugen. Somit kann, obwohl die erzeugten Drehmomente der Antriebe nicht als Messgröße vorliegen eine Aufteilung der Drehmomente erzielt werden.An advantageous solution provides that the first virtual setpoint speed and the second virtual setpoint speed are determined by means of a speed-torque characteristic of the fan wheel from the first torque and the second torque. On the basis of the known speed-torque characteristic, in short characteristic curve, it can be determined which speed the fan wheel would reach if the fan wheel is driven with the first or with the second torque. If this speed is used as the first setpoint speed or second virtual setpoint speed, due to the pilot control maps in the control units, the two drives which attempt to reach the virtual speeds generate just the first torque or the second torque. Thus, although the generated torques of the drives are not present as a measure, a distribution of the torques can be achieved.

Eine weitere vorteilhafte Lösung sieht vor, dass die erste Regeleinheit und die zweite Regeleinheit jeweils ein Vorsteuerkennfeld und einen PID-Regler verwenden. Diese Art der Regeleinheiten hat sich bewährt und ermöglicht eine schnelle und effiziente Regelung der Drehzahl des Lüfterrades.A further advantageous solution provides that the first control unit and the second control unit each use a pilot control map and a PID controller. This type of control units has proven itself and allows a fast and efficient control of the speed of the fan wheel.

In der Beschreibung und den beigefügten Ansprüchen wird unter einem PID-Regler ein Proportional-Integral-Differenzial-Regler verstanden.In the description and the appended claims, a PID controller is understood to mean a proportional-integral-derivative controller.

Eine besonders vorteilhafte Lösung sieht vor, dass die erste virtuelle Drehzahl als Eingangsgröße für das Vorsteuerkennfeld der ersten Regeleinheit des ersten Antriebs verwendet wird und dass die zweite virtuelle Soll-Drehzahl als Eingangsgröße für das Vorsteuerkennfeld der zweiten Regeleinheit des zweiten Antriebs verwendet wird. Durch die Verwendung der virtuellen Soll-Drehzahl als Eingangsgröße für die Vorsteuerkennfelder der Regeleinheiten werden aus den Vorsteuerkennfeldern gerade die Steuergrößen für die jeweiligen Antriebe bestimmt, welche notwendig sind, um die virtuellen Soll-Drehzahlen zu erreichen, also die Steuergrößen, die das erste Drehmoment bzw. das zweite Drehmoment durch die jeweiligen Antriebe erzeugen.A particularly advantageous solution provides that the first virtual speed is used as input to the pilot map of the first control unit of the first drive and that the second virtual target speed is used as an input to the pilot map of the second control unit of the second drive. By using the virtual target speed as an input variable for the pilot control maps of the control units are from the pilot control maps just determines the control variables for the respective drives, which are necessary to achieve the virtual target speeds, so the control variables that generate the first torque and the second torque through the respective drives.

Eine günstige Variante sieht vor, dass die Regelabweichung, welche von den PID-Reglern verwendet wird, aus einer Differenz zwischen der Drehzahl des Lüfterrades und der Soll-Drehzahl des Lüfterrades bestimmt wird. Auf diese Weise kann erzielt werden, dass die Regeleinheiten auf die richtige Soll-Drehzahl regeln, obwohl den Regeleinheiten die virtuellen Drehzahlen als Eingangsgröße zugeführt werden.A favorable variant provides that the control deviation, which is used by the PID controllers, from a difference between the speed of the fan and the target speed of the fan wheel is determined. In this way it can be achieved that the control units to the correct target speed control, although the control units, the virtual speeds are supplied as an input variable.

Eine weitere günstige Variante sieht vor, dass die jeweiligen Regelabweichungen, welche von den PID-Reglern verwendet werden, aus einer Differenz zwischen der jeweiligen virtuellen Soll-Drehzahl und einer jeweiligen virtuellen Ist-Drehzahl bestimmt werden. Die jeweiligen virtuellen Ist-Drehzahlen werden aus der Drehzahl des Lüfterrades in gleicher Weise gebildet wie die virtuellen Soll-Drehzahlen aus der Soll-Drehzahl, sodass bei einer Übereinstimmung der Drehzahl des Lüfterrades mit der Soll-Drehzahl auch die virtuellen Soll-Drehzahlen mit den virtuellen Ist-Drehzahlen übereinstimmen. Dadurch kann erreicht werden, dass die erste Regeleinheit und die zweite Regeleinheit das Lüfterrad auf die gewünschte Soll-Drehzahl regeln.A further favorable variant provides that the respective control deviations which are used by the PID controllers are determined from a difference between the respective virtual setpoint speed and a respective virtual actual speed. The respective virtual actual speeds are formed from the speed of the fan in the same way as the virtual target speeds from the target speed, so that at a match of the speed of the fan with the target speed and the virtual target speeds with the virtual Actual speeds match. It can thereby be achieved that the first control unit and the second control unit regulate the fan wheel to the desired desired speed.

Eine besonders günstige Variante sieht vor, dass die jeweiligen virtuellen Ist-Drehzahlen durch Subtraktion eines Offsets von der Drehzahl bestimmt werden, wobei das Offset die Differenz zwischen der Soll-Drehzahl und der jeweiligen virtuellen Soll-Drehzahl ist. Dadurch können durch einfache Addition- bzw. Subtraktionsrechnungen die virtuellen Ist-Drehzahlen bestimmt werden. Es ist also nur ein geringer Rechenaufwand notwendig.A particularly favorable variant provides that the respective virtual actual rotational speeds are determined by subtracting an offset from the rotational speed, wherein the offset is the difference between the target rotational speed and the respective virtual target rotational speed. As a result, the virtual actual rotational speeds can be determined by simple addition or subtraction calculations. So it is only a small amount of computation necessary.

Eine vorteilhafte Möglichkeit sieht vor, dass die virtuellen Ist-Drehzahlen durch Multiplikation der Drehzahlen mit einem Teilungsfaktor bestimmt werden, wobei der Teilungsfaktor der Quotient aus der jeweiligen virtuellen Soll-Drehzahl durch die Soll-Drehzahl ist. Auf diese Weise kann erreicht werden, dass derjenige Antrieb, welcher eine geringere Teilleistung leisten soll auch weniger stark an der Regelung der Drehzahl des Lüfterrades beteiligt ist, da durch die Multiplikation mit dem Teilungsfaktor entsprechend auch die Größe der Regelabweichung im Verhältnis zu der Leistungsaufteilung auf die jeweiligen Regeleinheiten aufgeteilt wird.An advantageous possibility provides that the virtual actual rotational speeds are determined by multiplying the rotational speeds by a division factor, wherein the division factor is the quotient of the respective virtual target rotational speed by the target rotational speed. In this way it can be achieved that the one drive, which is to perform a lower partial power and less involved in the control of the speed of the fan wheel, as by multiplication with the division factor according to the size of the control deviation in relation to the power distribution on the each control units is divided.

Eine vorteilhafte Lösung sieht vor, dass die erste Regeleinheit und die zweite Regeleinheit Drehzahlregeleinheiten sind, bzw. dass als erste Regeleinheit und als zweite Regeleinheit jeweils Drehzahlregeleinheiten verwendet werden. Drehzahlen können sehr leicht gemessen werden, so dass die Verwendung von Drehzahlregeleinheiten günstiger umzusetzen ist, als die Verwendung von Drehmomentregeleinheiten.An advantageous solution provides that the first control unit and the second control unit are speed control units, or that each speed control units are used as the first control unit and as the second control unit. Speeds can be measured very easily, so that the use of speed control units is cheaper to implement than the use of torque control units.

Eine weitere vorteilhafte Lösung sieht vor, dass die Drehzahlen des ersten Antriebs und des zweiten Antriebs gekoppelt sind. Der erste Antrieb und der zweite Antrieb können sich also nicht unabhängig voneinander drehen.A further advantageous solution provides that the rotational speeds of the first drive and the second drive are coupled. The first drive and the second drive can not rotate independently of each other.

Ferner wird die oben genannte Aufgabe durch ein Kraftfahrzeug mit einem Lüfter, der durch einen ersten Antrieb und durch einen zweiten Antrieb angetrieben ist gelöst, wobei eine Drehzahl mindestens eines Lüfterrades des Lüfters durch ein Verfahren gemäß der vorstehenden Beschreibung geregelt ist. Die Vorteile des Verfahrens übertragen sich somit auf das Kraftfahrzeug, auf deren vorstehende Beschreibung insoweit Bezug genommen wird.Furthermore, the above object is achieved by a motor vehicle with a fan, which is driven by a first drive and by a second drive, wherein a speed of at least one fan of the fan is controlled by a method as described above. The advantages of the method are thus transferred to the motor vehicle, to the above description of which reference is made.

Eine besonders günstige Variante sieht vor, dass der erste Antrieb ein Elektromotor ist und der zweite Antrieb eine Viscokupplung ist, welche das Lüfterrad an eine Brennkraftmaschine des Kraftfahrzeugs koppelt.A particularly favorable variant provides that the first drive is an electric motor and the second drive is a viscous coupling which couples the fan wheel to an internal combustion engine of the motor vehicle.

Weitere wichtige Merkmale und Vorteile der Erfindung ergeben sich aus den Unteransprüchen, aus den Zeichnungen und aus der zugehörigen Figurenbeschreibung anhand der Zeichnungen.Other important features and advantages of the invention will become apparent from the dependent claims, from the drawings and from the associated figure description with reference to the drawings.

Bevorzugte Ausführungsbeispiele der Erfindung sind in den Zeichnungen dargestellt und werden in der nachfolgenden Beschreibung näher erläutert, wobei sich gleiche Bezugszeichen auf gleiche oder ähnliche oder funktional gleiche Komponenten beziehen.Preferred embodiments of the invention are illustrated in the drawings and will be described in more detail in the following description, wherein like reference numerals refer to the same or similar or functionally identical components.

Es zeigen, jeweils schematisch.

Fig. 1
eine Prinzipskizze einer Anordnung umfassen eine Brennkraftmaschine und einen Lüfter mit einem ersten und einem zweiten Antrieb,
Fig. 2
ein Ablaufdiagramm eines Verfahrens zur Regelung einer Drehzahl eines Lüfterrades des Lüfters,
Fig. 3
eine Prinizipskizze einer Anordnung umfassend eine Brennkraftmaschine und einen Lüfter mit einem ersten und einem zweiten Antrieb, und
Fig. 4
ein Ablaufdiagramm eines Verfahrens zur Regelung der Drehzahl des Lüfterrades aus Fig. 3 gemäß einer zweiten Ausführungsform.
It show, each schematically.
Fig. 1
A schematic diagram of an arrangement comprises an internal combustion engine and a fan with a first and a second drive,
Fig. 2
a flowchart of a method for controlling a speed of a fan of the fan,
Fig. 3
a schematic diagram of an arrangement comprising an internal combustion engine and a fan with a first and a second drive, and
Fig. 4
a flowchart of a method for controlling the speed of the fan from Fig. 3 according to a second embodiment.

Eine in Fig. 1 dargestellte Anordnung 10 umfasst eine Brennkraftmaschine 12 mit einer Welle 14. Ferner umfasst die Anordnung einen Lüfter 16 mit mindestens einem Lüfterrad 17, welcher beispielsweise zur Kühlung der Brennkraftmaschine 12 eingesetzt wird. Und durch einen ersten Antrieb 18 und durch einen zweiten Antrieb 20 angetrieben wird.An in Fig. 1 Arrangement 10 includes an internal combustion engine 12 with a shaft 14. Furthermore, the arrangement comprises a fan 16 with at least one fan 17, which is used for example for cooling the internal combustion engine 12. And driven by a first drive 18 and by a second drive 20.

Der erste Antrieb 18 und der zweite Antrieb 20 unterscheiden sich, beispielsweise ist der erste Antrieb ein Elektromotor und der zweite Antrieb eine Viscokupplung, welche das Lüfterrad 17 mit der Welle 14 der Brennkraftmaschine 12 koppelt, sodass die Drehung der Welle 14 der Brennkraftmaschine 12 auf eine Drehung des Lüfterrades 17 übertragen wird.The first drive 18 and the second drive 20 differ, for example, the first drive is an electric motor and the second drive is a viscous coupling which couples the fan 17 with the shaft 14 of the internal combustion engine 12, so that the rotation of the shaft 14 of the internal combustion engine 12 to a Rotation of the fan 17 is transmitted.

Um eine Drehzahl 22 des Lüfterrades 17 zu regeln weist der erste Antrieb 18 eine erste Regeleinheit 24 und der zweite Antrieb 20 eine zweite Regeleinheit 26 auf. Die erste Regeleinheit 24 und die zweite Regeleinheit 26 regeln die Leistung des ersten Antriebs 18 bzw. des zweiten Antriebs 20 derart, dass sich die Drehzahl 22 des Lüfterrades 17 einer Soll-Drehzahl 28 zumindest annähert. Die Messung 23 der Drehzahl 22 kann beispielsweise durch einen Drehzahlmesser erfolgen.In order to regulate a rotational speed 22 of the fan wheel 17, the first drive 18 has a first control unit 24 and the second drive 20 has a second control unit 26. The first control unit 24 and the second control unit 26 regulate the power of the first drive 18 and the second drive 20 such that the rotational speed 22 of the fan wheel 17 at least approaches a target rotational speed 28. The measurement 23 of the speed 22 can be done for example by a tachometer.

Die Regeleinheiten 24, 26 weisen jeweils einen PID-Regler 25 (Proportional-Integral-Differenzial-Regler) und ein Vorsteuerkennfeld 27 auf. Ferner sind in dem Vorsteuerkennfeld 27 Steuergrößen 29 für die jeweiligen Antriebe hinterlegt, welche für bestimmte Betriebspunkte des Lüfters 16 notwendig sind. Beispielsweise sind Steuergrößen 29 für den stationären Betrieb abhängig von der Drehzahl 22 des Lüfterrades 17 hinterlegt. Bei Einstellen einer Soll-Drehzahl 28 an den Regeleinheiten 24, 26 kann mit Hilfe der Vorsteuerkennfelder 27 eine erste gute Schätzung für die richtigen Steuergrößen 29 für die Antriebe bestimmt werden, sodass die Annäherung an die tatsächlich benötigen Steuergrößen 29 schneller stattfinden kann.The control units 24, 26 each have a PID controller 25 (proportional-integral-differential controller) and a pilot control map 27. Furthermore, control variables 29 for the respective drives are stored in the pilot control map 27, which are necessary for certain operating points of the fan 16. For example, control variables 29 are stored for the steady-state operation as a function of the rotational speed 22 of the fan wheel 17. When setting a target speed 28 at the control units 24, 26 can be determined using the pilot control maps 27, a first good estimate for the correct control variables 29 for the drives, so that the approximation to the actual required control variables 29 can take place more quickly.

Eine Bestimmung 30 der Soll-Drehzahl 28 des Lüfterrades 17 erfolgt beispielsweise durch ein Motorsteuergerät 31, insbesondere anhand einer Temperatur der Brennkraftmaschine 12 oder einer Temperatur eines Kühlmediums, wie beispielsweise Wasser. Bei hohen Temperaturen werden höhere Soll-Drehzahlen gesetzt, um eine bessere Kühlung zu erhalten.A determination 30 of the setpoint speed 28 of the fan wheel 17 takes place, for example, by an engine control unit 31, in particular based on a temperature of the internal combustion engine 12 or a temperature of a cooling medium, such as water. At high temperatures, higher target speeds are set for better cooling.

Um einen möglichst guten Wirkungsgrad zu erzielen, wird eine Effizienzstrategie 32 angewendet. Die beiden Antriebe 18, 20 weisen unterschiedliche Wirkungsgrade insbesondere unterschiedliche Abhängigkeiten der Wirkungsgrade, beispielsweise von der Drehzahl oder des zu erzeugenden Drehmoments auf. Aus diesem Grund ist eine Leistungsaufteilung, welche für den Gesamtwirkungsgrad vorteilhaft ist, für verschiedene Betriebspunkte unterschiedlich. Dabei können verschiedene Fälle auftreten. In den zwei einfachsten Fällen übernimmt einer der Antriebe komplett das Antreiben des Lüfterrades 17, während der andere Antrieb keine Leistung erzeugt. Es gibt aber auch Fälle, bei denen eine Aufteilung der Leistungen für den Wirkungsgrad günstig ist, bei denen beide Antriebe 18, 20 zum Antreiben des Lüfterrades 17 beisteuern.In order to achieve the best possible efficiency, an efficiency strategy 32 is applied. The two drives 18, 20 have different efficiencies, in particular different dependencies of the efficiencies, for example, on the speed or the torque to be generated. For this reason, a power distribution which is advantageous for the overall efficiency is different for different operating points. There may be different cases. In the two simplest cases, one of the drives completely takes over the driving of the fan wheel 17, while the other drive does not generate power. But there are also cases in which a division of the benefits of the efficiency is low, in which both drives contribute 18, 20 for driving the fan wheel 17.

Der erste Antrieb 18 und der zweite Antrieb 20 treiben gemeinsam das Lüfterrad 17 an, sodass die Drehzahlen des ersten Antriebs 18 und des zweiten Antriebs 20 miteinander gekoppelt sind. Insbesondere sind die Drehzahlen des ersten Antriebs 18 und des zweiten Antriebs 20 gleich der Drehzahl 22 des Lüfterrades 17. Um eine Leistungsaufteilung zu erreichen, muss also das Drehmoment, welches notwendig ist um das Lüfterrad 17 anzutreiben auf die beiden Antriebe aufgeteilt werden. Der erste Antrieb 18 muss ein erstes Drehmoment 34 und der zweite Antrieb 20 muss ein zweites Drehmoment 36 aufbringen, um das Lüfterrad 17 auf die gewünschte Soll-Drehzahl 28 zu bringen.The first drive 18 and the second drive 20 jointly drive the fan 17, so that the rotational speeds of the first drive 18 and the second drive 20 are coupled together. In particular, the rotational speeds of the first drive 18 and the second drive 20 are equal to the speed 22 of the fan wheel 17. In order to achieve a power distribution, therefore, the torque which is necessary to drive the fan 17 must be divided between the two drives. The first drive 18 must have a first torque 34 and the second drive 20 must apply a second torque 36 to bring the fan 17 to the desired desired speed 28.

Für die Regelung der Drehzahl 22 des Lüfterrades 17 ist es allerdings problematisch, da die Drehmomente 34, 36, welche von den beiden Antrieben 18, 20, erzeugt werden nicht als Messgröße vorliegen und somit nicht als Regelgröße verwendet werden können.For the regulation of the rotational speed 22 of the fan wheel 17, however, it is problematic because the torques 34, 36, which are generated by the two drives 18, 20, are not present as a measured variable and thus can not be used as a controlled variable.

Das erste Drehmoment 34 und das zweite Drehmoment 36 werden in eine erste virtuelle Soll-Drehzahl 38 und eine zweite virtuelle Soll-Drehzahl 40 umgerechnet und als Eingangsgröße für die erste Regeleinheit 24 und die zweite Regeleinheit 26 verwendet.The first torque 34 and the second torque 36 are converted into a first target virtual speed 38 and a second target virtual speed 40 and used as input to the first control unit 24 and the second control unit 26.

Die Bestimmung der virtuellen Soll-Drehzahlen 38, 40 aus den Drehmomenten 34, 36 erfolgt mit Hilfe einer Drehmoment-Drehzahl-Kennlinie, kurz Kennlinie 41, des Lüfterrades 17. Diese Kennlinie 41 kann beispielsweise theoretisch aus der Geometrie des Lüfters 16 abgeleitet werden oder experimentell ermittelt werden. Aus der Kennlinie 41 sind die Drehmomente bekannt, welche notwendig sind, um das Lüfterrad 17 auf einer bestimmten Drehzahl zu halten. Entsprechend können aus der Kennlinie 41 die virtuellen Soll-Drehzahlen 38, 40 ermittelt werden, welche sich einstellen würden, wenn die beiden Antriebe 18, 20 mit dem aufgrund von der Effizienzstrategie 32 bestimmten ersten Drehmoment 34 und zweiten Drehmoment 36 das Lüfterrad 17 jeweils alleine antreiben würden.The determination of the virtual setpoint rotational speeds 38, 40 from the torques 34, 36 takes place with the aid of a torque / rotational speed characteristic, in short characteristic curve 41, of the fan wheel 17. This characteristic curve 41 can be derived, for example, theoretically from the geometry of the fan 16 or experimentally be determined. From the characteristic curve 41, the torques are known, which are necessary to keep the fan 17 at a certain speed. Accordingly, from the characteristic curve 41, the virtual setpoint rotational speeds 38, 40 can be determined, which would occur if the two drives 18, 20 with the first torque 34 and second torque 36 determined on the basis of the efficiency strategy 32 each drive the fan wheel 17 alone would.

Die virtuellen Drehzahlen 38, 40 werden als Eingangsgröße an die Regeleinheiten 24, 26 geleitet. In den Regeleinheiten 24 und 26 werden mit Hilfe der Vorsteuerkennfelder 27 die Steuergrößen 29 für die Antriebe 18, 20 bestimmt, die benötigt werden, um die Drehzahl 22 des Lüfterrades 17 auf den jeweiligen virtuellen Soll-Drehzahlen 38, 40 zu halten. Diese Steuergrößen 29 bewirken, dass die Antriebe 18, 20 die durch die Effizienzstrategie 32 bestimmten Drehmomente 34, 36 erzeugen. Somit erzeugen die beiden Antriebe 18 und 20 zu Beginn der Regelschleife das erste Drehmoment 34 und das zweite Drehmoment 36 genau in dem Verhältnis, das anhand der Effizienzstrategie 32 bestimmt wurde.The virtual speeds 38, 40 are passed as an input to the control units 24, 26. In the control units 24 and 26, the control variables 29 for the drives 18, 20 are determined with the aid of the pilot control maps 27, which are required to keep the rotational speed 22 of the fan wheel 17 at the respective virtual desired rotational speeds 38, 40. These control variables 29 cause the drives 18, 20 to determine the torques determined by the efficiency strategy 32 34, 36 generate. Thus, at the beginning of the control loop, the two drives 18 and 20 generate the first torque 34 and the second torque 36 exactly in the ratio determined by the efficiency strategy 32.

Zu Beginn der Regelschleife erfolgt eine Bestimmung 42 der Regelabweichung 44. Da den Regeleinheiten 24 und 26 virtuelle Soll-Drehzahlen 38, 40 zugeführt werden kann die Bestimmung 42 der Regelabweichung 44 nicht in der üblichen Art und Weise erfolgen, da ansonsten die beiden Antriebe 18, 20 jeweils auf eine unterschiedliche Drehzahl regeln würden, sodass die beiden Antriebe 18, 20 gegeneinander arbeiten würden.At the beginning of the control loop, a determination 42 of the control deviation 44 takes place. Since the control units 24 and 26 are supplied with virtual nominal rotational speeds 38, 40, the determination 42 of the control deviation 44 can not take place in the usual manner, since otherwise the two drives 18, 20 would each regulate to a different speed, so that the two drives 18, 20 would work against each other.

Die Bestimmung 42 der Regelabweichung 44 erfolgt daher durch die Bildung der Differenz zwischen der Soll-Drehzahl 28 und der Drehzahl 22 des Lüfterrades 17. Die Regelabweichung 44 wird dann beiden Regeleinheiten 24, 26 bereitgestellt, sodass die PID-Regler 25 der Regeleinheiten 24, 26 keine eigene Bestimmung 42 der Regelabweichung 44 durchführen müssen.The determination 42 of the control deviation 44 therefore takes place by forming the difference between the setpoint speed 28 and the speed 22 of the fan wheel 17. The control deviation 44 is then provided to both control units 24, 26, so that the PID controllers 25 of the control units 24, 26 do not have to make their own determination 42 of the control deviation 44.

Durch die Regelung des ersten Antriebs 18 und des zweiten Antriebs 20 können die beiden Antriebe 18, 20 sich von den Betriebspunkten entfernen, welche mit Hilfe der virtuellen Soll-Drehzahlen 38, 40 gesetzt wurden. Das heißt, dass das gewünschte Leistungsverhältnis, welches durch die Effizienzstrategie 32 bestimmt wurde, unter Umständen nicht eingehalten werden kann. Allerdings bleiben die Abweichungen gering, sodass die Anordnung 10 dennoch nahe dem Wirkungsgradoptimum betrieben werden kann.By controlling the first drive 18 and the second drive 20, the two drives 18, 20 can be removed from the operating points, which were set using the virtual target speeds 38, 40. That is, the desired power ratio determined by the efficiency strategy 32 may not be met. However, the deviations remain small, so that the arrangement 10 can still be operated close to the efficiency optimum.

Ferner wird bei einer Neufestlegung der Soll-Drehzahl 28 mit Hilfe der Effizienzstrategie 32 das richtige Leistungsverhältnis erneut eingestellt, sodass bei häufigen Soll-Drehzahlwechseln die Abweichung von dem gewünschten Leistungsverhältnis akzeptiert werden kann. Alternativ oder ergänzend hierzu kann auch vorgesehen sein, dass in einem bestimmten Intervall die Soll-Drehzahl 28 erneut gesetzt wird, obwohl keine Änderung der Soll-Drehzahl durch das Motorsteuergerät vorgesehen ist.Furthermore, when the setpoint speed 28 is redefined with the aid of the efficiency strategy 32, the correct power ratio is readjusted so that the deviation from the desired power ratio can be accepted for frequent setpoint speed changes. Alternatively or additionally, it can also be provided that setpoint speed 28 is set again in a specific interval is, although no change in the target speed is provided by the engine control unit.

Eine in den Fig. 3 und Fig. 4 dargestellte zweite Ausführungsform des Verfahrens zur Regelung der Drehzahl 22 des Lüfterrades 17 unterscheidet sich von der in der Fig. 1 und Fig. 2 dargestellten ersten Ausführungsform des Verfahrens dadurch, dass die Regelabweichung 44 innerhalb der Regeleinheiten 24, 26 aus einer Differenz zwischen den virtuellen Soll-Drehzahlen 38, 40 und virtuellen Ist-Drehzahlen 46 und 48 bestimmt wird. Dazu wird die Drehzahl 22 des Lüfterrades 17 umgerechnet in eine erste virtuelle Ist-Drehzahl 46 und in eine zweite virtuelle Ist-Drehzahl 48. Die erste virtuelle Ist-Drehzahl 46 wird dabei der ersten Regeleinheit 24 zugeführt und die zweite virtuelle Ist-Drehzahl 48 wird der zweiten Regeleinheit 26 zugeführt.One in the FIG. 3 and FIG. 4 illustrated second embodiment of the method for controlling the speed 22 of the fan 17 differs from that in the Fig. 1 and Fig. 2 shown in the method in that the control deviation 44 within the control units 24, 26 from a difference between the virtual target speeds 38, 40 and virtual actual speeds 46 and 48 is determined. For this purpose, the rotational speed 22 of the fan wheel 17 is converted into a first virtual actual rotational speed 46 and into a second virtual actual rotational speed 48. The first virtual actual rotational speed 46 is supplied to the first control unit 24 and the second virtual actual rotational speed 48 becomes the second control unit 26 is supplied.

Die Regelabweichung 44 wird dann in üblicher Weise in den Regeleinheiten 24, 26 durch Differenz zwischen der virtuellen Soll-Drehzahl und der virtuellen Ist-Drehzahl bestimmt. Auf diese Weise werden für die beiden Regeleinheiten 24, 26 unter Umständen unterschiedliche Regelabweichungen 44 ermittelt.The control deviation 44 is then determined in a conventional manner in the control units 24, 26 by the difference between the virtual target speed and the virtual actual speed. In this way, different control deviations 44 may be determined for the two control units 24, 26 under certain circumstances.

Zur Bestimmung 50 der virtuellen Ist-Drehzahlen 46, 48 sind grundsätzlich mehrere Möglichkeiten denkbar. Grundsätzlich müssen die virtuellen Ist-Drehzahlen 46, 48 derart aus der Drehzahl 22 des Lüfterrades 17 gebildet werden, dass wenn die Drehzahl 22 des Lüfterrades 17 der Soll-Drehzahl 28 entspricht, die erste virtuelle Ist-Drehzahl 46 der ersten virtuellen Soll-Drehzahl 28 und die zweite virtuelle Ist-Drehzahl 48 der zweiten virtuellen Soll-Drehzahl 40 entsprechen. Dadurch kann sichergestellt werden, dass die beiden Regeleinheiten 24, 26 die Drehzahl 22 des Lüfterrades 17 gemeinsam auf die Soll-Drehzahl 28 regeln.In principle, several possibilities are conceivable for determining 50 the virtual actual rotational speeds 46, 48. In principle, the virtual actual rotational speeds 46, 48 must be formed from the rotational speed 22 of the fan wheel 17 such that when the rotational speed 22 of the fan wheel 17 corresponds to the target rotational speed 28, the first virtual actual rotational speed 46 of the first virtual target rotational speed 28 and the second actual virtual speed 48 correspond to the second target virtual speed 40. This can ensure that the two control units 24, 26 control the speed 22 of the fan 17 together to the target speed 28.

Eine erste Möglichkeit, die virtuellen Ist-Drehzahlen 46, 48 zu bestimmen, besteht darin, die Differenz zwischen der Soll-Drehzahl 28 und den virtuellen Soll-Drehzahlen 38, 40 von der Drehzahl 22 des Lüfterrades 17 abzuziehen. Wie beispielsweise durch folgende Formel beschrieben: virtuelle Ist Drehzahl = Drehzahl Soll Drehzahl virtuelle Soll Drehzahl

Figure imgb0001
A first way to determine the virtual actual speeds 46, 48 is to calculate the difference between the desired speed 28 and the virtual target speeds 38, 40 subtract from the speed 22 of the fan 17. As described for example by the following formula: virtual is - rotation speed = rotation speed - Should - rotation speed - virtual target - rotation speed
Figure imgb0001

Bei einer weiteren Möglichkeit zur Bestimmung 50 der virtuellen Ist-Drehzahlen 46, 48 wird das gleiche Verhältnis zwischen der Drehzahl 22 und den virtuellen Ist-Drehzahlen 46, 48 eingehalten wie zwischen der Soll-Drehzahl 28 und den virtuellen Soll-Drehzahlen 38, 40. Dieses Verhalten kann beispielsweise durch folgende Formel beschrieben werden: Virtuelle Ist Drehzahl = Drehzahl * virtuelle Soll Drehzahl / Soll Drehzahl

Figure imgb0002
In a further possibility for determining 50 of the virtual actual rotational speeds 46, 48, the same ratio between the rotational speed 22 and the virtual actual rotational speeds 46, 48 is maintained as between the desired rotational speed 28 and the virtual nominal rotational speeds 38, 40. This behavior can be described by the following formula, for example: Virtual Actual - rotation speed = rotation speed * virtual target - rotation speed / Should - rotation speed
Figure imgb0002

Beide aufgezählten Varianten ermöglichen es, dass beide Regeleinheiten 24, 26 gemeinsam arbeiten und die Drehzahl 22 des Lüfterrades 17 auf die Soll-Drehzahl 28 regeln. Andere Möglichkeiten zur Bestimmung 50 der virtuellen Ist-Drehzahl 46, 48 sind ebenfalls denkbar, solange die virtuellen Ist-Drehzahlen 46, 48 mit den virtuellen Soll-Drehzahlen 38, 40 übereinstimmen, wenn die Drehzahl 22 mit der Soll-Drehzahl 28 übereinstimmt. Im Übrigen stimmt die in den Fig. 3 und Fig. 4 dargestellte zweite Ausführungsform des Verfahrens hinsichtlich Ablauf und Funktion mit der in den Fig. 1 und Fig. 2 dargestellten ersten Ausführungsform des Verfahrens überein, auf deren vorstehende Beschreibung insoweit Bezug genommen wird.Both enumerated variants make it possible for both control units 24, 26 to work together and to regulate the rotational speed 22 of the fan wheel 17 to the desired rotational speed 28. Other possibilities for determining 50 of the virtual actual rotational speed 46, 48 are also conceivable as long as the virtual actual rotational speeds 46, 48 coincide with the virtual target rotational speeds 38, 40 when the rotational speed 22 coincides with the target rotational speed 28. Incidentally, the right in the FIG. 3 and FIG. 4 illustrated second embodiment of the method with regard to sequence and function with in the Fig. 1 and Fig. 2 illustrated first embodiment of the method, to the above description, reference is made in this regard.

Claims (14)

  1. Method for regulating a rotational speed (22) of a fan wheel (17) to a target rotational speed (28), said fan wheel being driven jointly by a first drive (18) and a second drive (20), wherein the first drive (18) is regulated and/or controlled by a first regulating unit (24) and the second drive (20) is regulated and/or controlled by a second regulating unit (26),
    characterised in that
    - a first torque (34) to be generated by the first drive (18) and a second torque (36) to be generated by the second drive (20) are determined based on an efficiency strategy (32),
    - a first virtual target rotational speed (38) and a second virtual target rotational speed (40) are determined starting from the first torque (34) and the second torque (36),
    - the first virtual target rotational speed (38) is supplied to the first regulating unit (24) as an input variable, and
    - the second virtual target rotational speed (40) is supplied to the second regulating unit (26) as an input variable.
  2. Method according to claim 1,
    characterised in that
    an electric motor is used as a first drive (18) and a viscous coupling as a second drive (20) which couples the fan wheel (17) to a shaft (14) of an internal combustion engine (12).
  3. Method according to claim 1 or 2,
    characterised in that
    the torques (34, 36) to be generated by the first drive (18) and by the second drive (20) are determined by the efficiency strategy (32) based on a target rotational speed (28) of the fan wheel (17) and/or a rotational speed of the internal combustion engine (12).
  4. Method according to any one of claims 1 to 3,
    characterised in that
    the torques (34, 36) to be generated by the first drive (18) and by the second drive (20) are determined by the efficiency strategy (32) taking into account the efficiency level of the first drive (18) and of the second drive (20).
  5. Method according to any one of claims 1 to 4,
    characterised in that
    the first virtual rotational speed (38) and the second virtual target rotational speed (40) are determined, using a speed-torque characteristic curve (41) of the fan wheel (17), from the first torque (34) and the second torque (36).
  6. Method according to any one of claims 1 to 5,
    characterised in that
    the first regulating unit (24) and the second regulating unit (26) respectively use a pilot control characteristic diagram (27) and a PID controller (25).
  7. Method according to claim 6,
    characterised in that
    the first virtual target rotational speed (38) is used as the input variable for the pilot control characteristic diagram (27) of the first regulating unit (24) of the first drive (18), and the second virtual target rotational speed (40) is used as the input variable for the pilot control characteristic diagram (27) of the second regulating unit (26) of the second drive (20).
  8. Method according to claim 6 or 7,
    characterised in that
    the control deviation (44) used by the PID controllers (25) is determined from a difference between the rotational speed (22) of the fan wheel (17) and the target rotational speed (28) of the fan wheel (17).
  9. Method according to claim 6 or 7,
    characterised in that
    the respective control deviations (44) used by the PID controllers (25) are determined from a difference between the respective virtual target rotational speed (38, 40) and a respective virtual actual rotational speed (46, 48).
  10. Method according to claim 9,
    characterised in that
    - the respective virtual actual rotational speeds (46, 48) are determined by subtraction of an offset from the rotational speed (22), wherein the offset is the difference between the target rotational speed (28) and the respective virtual target rotational speed (38, 40).
    - the virtual actual rotational speeds (46, 48) are determined by multiplication of the rotational speed (22) with a division factor, wherein the division factor is the quotient of the respective virtual target rotational speed (38, 40) by the target rotational speed (28).
  11. Method according to any one of claims 1 to 10,
    characterised in that
    the first regulating unit (24) and the second regulating unit (26) are rotational speed regulating units.
  12. Method according to any one of claims 1 to 11,
    characterised in that
    the rotational speeds of the first drive and of the second drive are coupled.
  13. Motor vehicle with a fan (16) driven jointly by a first drive (18) and by a second drive (20), wherein a rotational speed (22) of the fan wheel (17) of the fan (16) is regulated by a method according to any one of claims 1 to 12.
  14. Method according to claim 13,
    characterised in that
    the first drive (18) is an electric motor and the second drive (20) is a viscous coupling which couples the fan wheel (17) to an internal combustion engine (12) of the motor vehicle.
EP16151537.4A 2015-01-20 2016-01-15 Method for controlling a rotational speed of a fan Not-in-force EP3048307B1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102015200856.8A DE102015200856A1 (en) 2015-01-20 2015-01-20 Method for controlling a speed

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EP3048307B1 true EP3048307B1 (en) 2017-08-02

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Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4212984C2 (en) * 1992-02-07 1995-07-06 Man Nutzfahrzeuge Ag Motor vehicle with an internal combustion engine which can be charged by means of an exhaust gas turbocharger and a hydrostatic-mechanical drive for the auxiliary units
DE10219872A1 (en) 2002-05-03 2003-11-20 Behr Gmbh & Co Fan drive, especially for vehicle, with liquid friction clutch has rotor of additional electrical drive made integrally with fan drive that is directly associated with clutch housing
DE102005061414A1 (en) * 2005-12-22 2007-06-28 Robert Bosch Gmbh Operating hybrid vehicle with first electrical machine revolution rate regulated and second torque regulated, at least some of the tim, involves operating internal combustion engine by regulating its revolution rate
DE102006045502A1 (en) * 2006-09-27 2008-04-03 Jungheinrich Ag Device for controlling a hybrid drive system for a motor vehicle, in particular an industrial truck
DE102007046665A1 (en) * 2007-09-27 2009-04-02 Behr Gmbh & Co. Kg Speed control device for a clutch for driving a machine, system of speed control device and a higher-level control, control clutch, turbomachine, cooling system and method for speed control for a clutch for driving a machine
CN104895661A (en) * 2009-10-17 2015-09-09 博格华纳公司 Hybrid fan drive with electric motor
WO2012103431A1 (en) * 2011-01-27 2012-08-02 The Timken Company Variable speed compressor and control system
DE102012216337A1 (en) * 2011-09-14 2013-03-14 Behr Gmbh & Co. Kg Fluid friction coupling for fan wheel of internal combustion engine of e.g. pickup truck, has electric drive unit whose stator is attached to actuator assembly, and rotor is rotatably arranged on secondary module

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
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